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Optical Performance Assessment under Environmental and Mechanical Perturbations in Large, Deployable Telescopes

机译:大型可展开望远镜在环境和机械扰动下的光学性能评估

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Prediction of optical performance for large, deployable telescopes under environmental conditions and mechanical disturbances is a crucial part of the design verification process of such instruments for all phases of design and operation: ground testing, commissioning, and on-orbit operation. A Structural-Thermal-Optical-Performance (STOP) analysis methodology is often created that integrates the output of one analysis with the input of another. The integration of thermal environment predictions with structural models is relatively well understood, while the integration of structural deformation results into optical analysis/design software is less straightforward. A Matlab~® toolbox has been created that effectively integrates the predictions of mechanical deformations on optical elements generated by, for example, finite element analysis, and computes optical path differences for the distorted prescription. The engine of the toolbox is the real ray-tracing algorithm that allows the optical surfaces to be defined in a single, global coordinate system thereby allowing automatic alignment of the mechanical coordinate system with the optical coordinate system. Therefore, the physical location of the optical surfaces is identical in the optical prescription and the finite element model. The application of rigid body displacements to optical surfaces, however, is more general than for use solely in STOP analysis, such as the analysis of misalignments during the commissioning process. Furthermore, all the functionality of Matlab~® is available for optimization and control. Since this is a new tool for use on flight programs, it has been verified against CODE V. The toolbox' functionality, to date, is described, verification results are presented, and, as an example of its utility, results of a thermal distortion analysis are presented using the James Webb Space Telescope (JWST) prescription.
机译:在环境条件和机械干扰下,大型可部署望远镜的光学性能的预测是此类仪器在设计和运行的所有阶段(地面测试,调试和在轨运行)的设计验证过程的关键部分。通常创建一种结构热光学性能(STOP)分析方法,该方法将一种分析的输出与另一种分析的输入集成在一起。热环境预测与结构模型的集成相对较容易理解,而将结构变形结果集成到光学分析/设计软件中则不太直接。已经创建了Matlab®工具箱,该工具箱有效地集成了通过例如有限元分析生成的光学元件的机械变形的预测,并计算了扭曲处方的光程差。工具箱的引擎是真正的光线跟踪算法,该算法允许在单个全局坐标系中定义光学表面,从而使机械坐标系与光学坐标系自动对齐。因此,光学处方和有限元模型中光学表面的物理位置相同。但是,将刚体位移应用于光学表面比将其仅用于STOP分析(例如调试过程中的未对准分析)更为普遍。此外,Matlab〜®的所有功能均可用于优化和控制。由于这是一种用于飞行程序的新工具,因此已针对CODE V进行了验证。迄今为止,该工具箱的功能已得到描述,并提供了验证结果,并以其实用性为例,介绍了热变形的结果。使用James Webb太空望远镜(JWST)处方进行分析。

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